View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 63712U 26145.38859348 +.00000000 +00000-0 +48961-3 0 00009
2 63712 53.1591 223.2191 0001806 85.8407 274.2801 15.31720294 00
| Epoch (UTC): | 25 May 2026 09:19:34 |
| Eccentricity: | 0.0001806 |
| inclination: | 53.1591° |
| perigee height: | 469 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 223.2191° |
| argument of perigee: | 85.8407° |
| revolutions per day: | 15.31720294 |
| mean anomaly at epoch: | 274.2801° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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